File:Apollo_14_Lunar_Module_(LM)_on_the_moon.jpg · Wikimedia Commons · See Wikimedia Commons
Key facts
- Manufacturer
- Grumman
- Designer
- Thomas J. Kelly
- Country of origin
- United States
- Operator
- NASA
- Applications
- Crewed lunar landing
- Spacecraft type
- Lunar lander
- Launch mass
- 33,500 lb (15,200 kg) standard 36,200 lb (16,400 kg) extended
- Dry mass
- 9,430 lb (4,280 kg) standard 10,850 lb (4,920 kg) extended
- Volume
- 235 ft (6.7 m )
- Power
- 28 V DC, 115 V 400 Hz AC
- Batteries
- Six or seven 28–32-volt, 296-416 ampere hour silver zinc battery
- Regime
- Lunar orbit Lunar landing
- Design life
- 75 hours (extended)
- Length
- 23 ft 1 in (7.04 m)
- Diameter
- 13 ft 10 in (4.22 m) without landing gear
- Width
- 31 ft (9.4 m), landing gear deployed
- Status
- Retired
- Maiden launch
- January 22, 1968
via Wikipedia infobox
Wikidata facts
- Subclass of
- lunar lander
- Part of
- Apollo
- Operator
- NASA
- Country of origin
- United States
- Diameter
- 4.27
- Mass
- 4280
- Manufacturer
- Grumman
- Image
- Apollo 11 Lunar Lander - 5927 NASA.jpg
- Height
- 7
- Has use
- Moon landing
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Sources (2)
via Wikidata · CC0